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AFI 11-246v1_Aerial - Check six

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30 <strong>AFI</strong><strong>11</strong>-246V1 22 NOVEMBER 2002<br />

Table 3.4. A-10 Four-Point Roll Parameters.<br />

TARGET PARAMETERS<br />

Altitude AGL Airspeed KCAS Power<br />

G<br />

Setting<br />

Entry 500’ 350 MAX +1 to –1<br />

Exit 500’ 350 MAX 1<br />

Altitude AGL<br />

PARAMETER LIMITS<br />

Airspeed KCAS<br />

MIN/MAX<br />

3.10.1. Maneuver Description . Entry to the Four-Point roll can either be initiated using a Split ìSî<br />

or Sliceback maneuver from the perch point achieved from the Show entry maneuver. A pull up of 5.0<br />

to 6.0 Gs is initiated from either maneuver at 1,200 feet AGL to arrive on the 1,500-foot show line at<br />

500 feet AGL and 350 knots. 2,000 feet prior to show center, pull the nose 3 to 5 degrees nose high,<br />

establish a climb, and unload. A cadence four-point roll to the left is then performed by pausing<br />

momentarily at the 90-degree, 180-degree, 270-degree, and 360-degree points. The pace of the<br />

cadence should ensure the aircraft is at the 180-degree point over show center. In order to facilitate<br />

sharp transitions between each 90 degrees of roll, momentarily ìfanî the speed brakes and unload the<br />

aircraft to 0 Gs at the initiation of each roll. Be sure to close the speed brakes upon completion of the<br />

roll to avoid any unnecessary loss of airspeed. The 90-degree and 270-degree points require top rudder<br />

to maintain level flight and zero G to maintain the show line. The 180-degree point requires 1 negative<br />

G in order to maintain level flight. This is accomplished using the horizon, not the G meter. At<br />

the completion of the Four-Point Roll, begin the Cuban 8 (high show) or 360-degree level turn (low<br />

show).<br />

3.10.2. Abnormal Procedures: If at anytime during the Four-Point Roll, the nose falls more than<br />

five degrees below the horizon, abort by rolling towards the nearest horizon and a wings-level position,<br />

then continue down the show line. This would most likely occur during the 3 rd point (270<br />

degrees) due to a decrease in airspeed, which results in less rudder effectiveness.<br />

3.<strong>11</strong>. Cuban 8 (Right to Left--High Profile Only).<br />

Power<br />

Setting<br />

Entry min 400’ 290 AC LMT MAX N/A<br />

Exit min 400’ 290 AC LMT MAX N/A<br />

G

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